US10184526B2 - Constant velocity joint boot assembly - Google Patents
Constant velocity joint boot assembly Download PDFInfo
- Publication number
- US10184526B2 US10184526B2 US15/404,919 US201715404919A US10184526B2 US 10184526 B2 US10184526 B2 US 10184526B2 US 201715404919 A US201715404919 A US 201715404919A US 10184526 B2 US10184526 B2 US 10184526B2
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- Prior art keywords
- boot
- sleeve
- axial
- axial length
- constant velocity
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
- F16D3/84—Shrouds, e.g. casings, covers; Sealing means specially adapted therefor
- F16D3/843—Shrouds, e.g. casings, covers; Sealing means specially adapted therefor enclosed covers
- F16D3/845—Shrouds, e.g. casings, covers; Sealing means specially adapted therefor enclosed covers allowing relative movement of joint parts due to the flexing of the cover
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J3/00—Diaphragms; Bellows; Bellows pistons
- F16J3/02—Diaphragms
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
- F16D3/16—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts
- F16D3/20—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts one coupling part entering a sleeve of the other coupling part and connected thereto by sliding or rolling members
- F16D3/22—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts one coupling part entering a sleeve of the other coupling part and connected thereto by sliding or rolling members the rolling members being balls, rollers, or the like, guided in grooves or sockets in both coupling parts
- F16D3/223—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts one coupling part entering a sleeve of the other coupling part and connected thereto by sliding or rolling members the rolling members being balls, rollers, or the like, guided in grooves or sockets in both coupling parts the rolling members being guided in grooves in both coupling parts
Definitions
- the device described herein relates to a boot assembly for a constant velocity joint.
- Boots are well-known devices used to enclose an end of a constant velocity joint. Boots keep out dirt, debris and moisture from the joint and keep lubricant in the joint.
- FIG. 1 One example of a prior art boot 10 for a joint 12 is depicted in FIG. 1 .
- the joint 12 comprises an inner race 14 , an outer race 16 , a cage 18 and at least one ball 20 within the cage 18 .
- the boot 10 encloses one end of the joint 12 .
- the boot 10 is connected at one end to the outer race 16 with a boot can 22 .
- a boot bead 26 is formed on the boot can 22 to capture the boot 10 .
- the boot bead 26 is generally round and formed inwardly.
- a boot can crimp 28 also helps hold the boot 10 in place.
- the boot can crimp 28 is also formed inwardly.
- the boot 10 is connected at the other end to a shaft 24 , such as by a clamp 30 .
- boot length L The size of the boot 10 used in FIG. 1 is characterized by boot length L, boot can length LL, boot can inner diameter ⁇ Db and the thickness of the boot 10 .
- Boot length L, boot can length LL and boot can inner diameter ⁇ Db are determined by the required maximum static articulation angle capability, which is depicted in FIG. 2 . More particularly, boot length L is determined in a way that boot length L in a joint assembly state as shown in FIG. 1 is equivalent to the boot length of an extended boot region 32 and the boot length of a contracted boot region 34 at a maximum joint angle.
- Boot thickness for the boot 10 of FIGS. 1 and 2 is depicted in FIG. 3 .
- The-boot 10 generally has a round shape RR with an angle ⁇ from the horizontal, where the thickness T 1 of an upper slope portion 36 , is equal to the thickness T 2 of a concave portion 38 , which is equal to the thickness T 3 of a lower slope portion 40 .
- the joint boot thickness T 2 , T 2 , T 3 is determined by taking into consideration boot radial and axial stiffness related to potential high risk boot failure modes, such as boot inversion and boot folding, both of which mainly occur at high joint internal pressures.
- Line ⁇ Dg represents the typical grease fill level for such a joint 12 .
- FIGS. 4-8 depict another prior art constant velocity joint 42 with a boot 44 .
- the joint 42 comprises an inner race 46 , an outer race 48 , a cage 50 and at least one ball 52 within the cage.
- This joint 42 uses a sleeve 54 that couples the inner race 46 with a pinion shaft 56 .
- a nut 58 connects the sleeve 54 to the pinion shaft 56 .
- the sleeve 54 in such a direct pinion mount design has a larger diameter Ds 1 than a tube shaft diameter Ds in a non-direct pinion mount design, such as shown in FIGS. 1-3 . Therefore, the boot can inner diameter Db 1 should increase by the difference between Ds 1 -Ds to have the equivalent maximum static joint angle capability to that of a non-direct pinion mount design, such as in FIGS. 1-3 . This results in a higher grease pressure acting on the direct pinion mount boot 44 compared with the pressure on the boot 10 depicted in FIG. 1 .
- the boot length L 1 is limited by the nut 58 as shown in FIG. 4 , therefore, it is more difficult to make the boot length L 1 equivalent to the non-direct pinion mount joint boot length L depicted in FIG. 1 .
- the limited boot axle length L 1 cannot provide a sufficient press fit contact portion 62 between the sleeve 54 and the boot 44 , which causes region 64 near a boot groove seat 66 to be bumped up and tilted toward the boot groove seat 66 by a crimping force of a boot clamp 68 acting on the boot clamp seat inside corner 70 , which can be appreciated from FIGS. 6 and 7 .
- the figure also depicts the boot 44 being severely bent at an edge of the boot can crimp 80 by high grease pressure while operating at a high temperature, a high operating speed and at a high operating angle.
- a constant velocity joint boot assembly has a boot can with a first end portion connected to an outer race and a second end portion cantilevered from the outer race.
- the second end portion has a planar portion extending from the first end portion at an angle.
- a radially outward extending end extends from the planar portion.
- a boot has a first end and a second end. The first end has an inner surface that is directly connected to an inner surface of the planar portion of the boot can.
- a sleeve has one end portion connected to an inner surface of an inner race with complementary splines and a second end portion extending axially away from the inner race. The boot has a lower portion engaged with the sleeve.
- FIG. 1 is a partial side view cross section of a first prior art constant velocity joint
- FIG. 2 is a partial side view cross section of a portion of the joint of FIG. 1 at a maximum articulation angle
- FIG. 3 is a partial side view cross section of a portion of the joint of FIG. 1 ;
- FIG. 4 is a second partial side view cross section of a prior art constant velocity joint
- FIG. 5 is a partial side view cross section of a portion of the joint of FIG. 4 at a maximum articulation angle
- FIG. 6 is a partial side view cross section of a portion of the joint of FIG. 4 ;
- FIG. 7 is a partial side view cross section of a portion of the joint of FIG. 4 ;
- FIG. 8 is a partial side view cross section of a portion of the joint of FIG. 4 ;
- FIG. 9 is a partial side view cross section of a first embodiment of a constant velocity joint and boot system
- FIG. 10 is a partial side view cross section of a portion of the joint in FIG. 9 ;
- FIGS. 10A-10C are partial side view cross-sections of portions of the joint in FIG. 9 ;
- FIG. 11 is a partial side view cross section of a second embodiment of a constant velocity joint and boot system
- FIG. 12 is a partial side view cross section of a third embodiment of a constant velocity joint
- FIG. 12A is a partial side view cross section of a detail of the joint in FIG. 12 ;
- FIG. 13 is a partial side-view cross section of a fourth embodiment of a constant velocity joint and boot system
- FIGS. 14A-14C comprises three partial side view cross sections of portions of the joint in FIG. 13 ;
- FIG. 15 is a partial side view cross section of a fifth embodiment of a constant velocity joint and boot system
- FIG. 16 is a partial side view cross section of a sixth embodiment of a constant velocity joint and boot system
- FIG. 17 is a partial side view cross section of a seventh embodiment of a constant velocity joint boot system
- FIG. 17A is a partial side view cross section of a detail from FIG. 17 ;
- FIG. 18 is a partial side view cross section of an eighth embodiment of a constant velocity joint boot system
- FIG. 19 is a partial side view cross section of a ninth embodiment of a constant velocity joint boot system.
- FIG. 19A is a partial side view cross section of a detail from FIG. 19 .
- FIG. 9 one embodiment of a boot system 82 for a direct pinion mount joint 84 is depicted.
- the joint 84 comprises an inner race 86 , an outer race 88 , a cage 90 and at least one ball 92 within the cage 90 .
- a tube 94 is connected, such as by welding, to the outer race 88 .
- a first end 96 of a sleeve 98 is connected, such as by splines 100 , to the inner diameter of the inner race 86 .
- a second end 102 of the sleeve 98 receives a pinion shaft 104 therein, such as through a splined connection 106 .
- a nut 108 connects the pinion shaft 104 to the sleeve 98 .
- a boot can 110 is depicted in FIGS. 9 and 10 .
- the boot can 110 has a first end portion 112 connected to the outer race 88 and a second end portion 114 that is cantilevered over the joint 84 . More particularly, the second end portion 114 is cantilevered over a portion of the sleeve 98 .
- the second end portion 114 comprises an outwardly angled, planar portion 116 and a boot can crimp head 118 at an end of the angled, planar portion 116 .
- the boot can crimp head 118 first extends radially outward from the angled, planar portion 116 before it curves around on itself to create a semi-hemispherical hollow portion 120 .
- a boot bead 121 is located in the portion 120 .
- the boot bead 121 has an outward radially extending portion with a complementary shape to the portion 120 .
- One end 122 of a straight portion 124 of the can 110 connects with the semi-hemispherical hollow portion 120 .
- the boot can 110 terminates at the other end 126 of the straight portion 124 .
- the straight portion 124 is located radially inward from the angled, planar portion 116 .
- a gap 128 separates the angled, planar portion from the straight portion 124 .
- the boot thickness smoothly decreases from an upper slope region 130 , through a concave region 132 down to a lower slope region 134 .
- the range of thicknesses of the upper slope region may be generally designated as T 31
- the range of thicknesses of the concave region 132 may be designated T 32
- the range of thicknesses of the lower slope region 134 may be generally designated as T 33 .
- the decrease in thickness is represented by T 31 >T 32 >T 33 .
- the decrease in thickness from the upper slope region 130 to the lower slope region 134 reduces boot radial deformation caused by high grease pressure anywhere in the boot 136 , but is particularly effective at the upper slope region 130 .
- the boot 136 also includes a boot stopper 138 in the upper slope region 130 , as shown in FIG. 10A . More particularly, the boot stopper 138 is located on an outside boot surface 140 that abuts, or is adjacent, the boot can straight portion 124 . The boot stopper 138 comprises a radially inward step 142 into the boot 136 that reduces the thickness of the boot 136 at that location of the step 142 . The boot stopper 138 prevents radial boot deformation via the direct contact with the boot can 110 , particularly when the boot 136 is significantly deformed.
- a press load ⁇ 2 is used to locate the upper slope region 130 into the boot can crimp head 118 .
- the press load ⁇ 2 functions to minimize boot radial deformation.
- Lower slope region 134 transitions to a boot clamping portion 143 , as shown in FIG. 10B .
- the boot clamping portion 143 comprises three portions: L 3 (as shown in FIG. 10A ), L 41 , and L 42 .
- L 3 comprises a planar portion 144 on an inside surface 146 of the boot 136 .
- a press load ⁇ 1 is applied to L 3 so that L 3 is located in contact with the sleeve 98 .
- the press load ⁇ 1 also minimizes the effect, if any, of an inside corner 148 of a boot seat groove 150 that can function like a hinge on the boot 136 to lift it away from the sleeve 98 .
- a clamp 151 is located in the boot seat groove 150 .
- the upper slope portion, the concave region and the lower slope region form a C-shape.
- the upper slope region is radially above the lower slope region and/or the boot clamping portion.
- a portion of the boot clamping portion extends axially beyond the upper slope region. More particularly, the boot seat groove extends axially beyond the upper slope region.
- a first angled transition 152 in the boot 136 separates L 3 from L 41 and L 42 .
- the first angled transition 152 has a complementary shape to a first angled transition 154 in an outer surface 156 of the sleeve 98 .
- the first angled transition extends into the sleeve 98 at a radial angle.
- the first angled transition 154 in the sleeve 98 leads to a sleeve groove 158 .
- the sleeve groove 158 is planar.
- a second angled transition 160 extends from the sleeve groove 158 .
- the second angled transition 160 extends into the sleeve 98 at a radial angle.
- L 41 and L 42 are coplanar surfaces with one another on the inside surface 146 of the boot 136 .
- L 41 is designed to be longer than L 42 ; the two lengths being separated by line Y-Y which defines a centerline of the boot seat groove 150 and the clamp 151 .
- L 41 is longer than L 42 to reduce or prevent region 162 from being lifted and tilted by the above-mentioned corner 148 .
- the thickness of the region 162 is gradually reduced from the general range of thicknesses in the region of T 35 to the general range of thicknesses in the region of T 36 along L 3 . The reduction in thickness also reduces or prevents the region 162 from being lifted and tilted by the corner 148 .
- a second angled transition 164 in the boot 136 which is complementary to transition 160 , connects L 42 with a boot end portion 166 .
- L 41 and L 42 are parallel to the sleeve groove 158 and L 41 and L 42 are equal length compared with sleeve groove 158 . And, upon application of a clamping force by the clamp 151 , L 41 and L 42 come into contact with the sleeve groove 158 . Similarly, the first and second angled transitions 152 , 164 in the boot 136 come into contact with the first and second angled-transitions 154 , 160 in the sleeve 98 upon application of the clamping force.
- FIG. 11 a second embodiment of a boot system 168 for the direct pinion joint 84 is depicted.
- the components of the joint 84 and the components of the boot system 168 are the same as those depicted in the first embodiment, except as follows.
- the straight portion 124 is oriented parallel to a joint center line X-X to improve manufacturability of the boot can 120 and the crimp head 168 in the can 120 by controlling the boot can inner diameter Db 1 .
- the straight portion 124 does not abruptly terminate as in the first embodiment. Instead, a radiused end portion 172 that extends radially inward from the boot 136 is used.
- FIGS. 12 and 12A depict a third embodiment of a boot system 174 for the direct pinion mount joint 84 .
- the components of the joint 84 and the components of the boot system 174 are the same as those depicted in the first embodiment, except as follows.
- a boot 176 in FIGS. 12 and 12A has a semi-half rectangular cross section that has a thickness that gradually and smoothly decreases from an upper slope region 178 through a concave region 180 down to a lower slope region 182 .
- the thickness T 41 of the upper slope region 178 is greater than the thickness T 42 of the concave region 180 , which is greater than the thickness T 43 of the lower slope region 182 .
- the boot 176 has a straight portion L 8 between the upper slope region 178 and the lower slope region 182 .
- the straight portion L 8 may be on one or both sides of the boot 176 . While FIGS. 12 and 12A depict L 8 as having one length, other lengths are permissible.
- the straight portion L 8 is designed to maintain grease pressure in the joint 84 .
- the straight portion may have a thickness T 42 that is substantially constant in order to maintain the grease pressure.
- FIGS. 13 and 14A-14C depict a fourth embodiment of a boot system 184 for the direct pinion mount joint 84 .
- the boot can crimp head 118 depicted and described in the previous embodiments is removed from the boot can 186 .
- the boot can 186 has the second end portion 114 with an angled, planar portion 116 .
- the boot can angled, planar portion 116 terminates in a radiused, radially outward extending end 188 .
- the boot can angled, planar portion 116 extends for a length L 7 .
- An inner surface 190 of the boot 192 is directly bonded or vulcanized to an inner surface 194 of the boot can 186 along the boot can angled, planar portion 116 at least partially along L 7 .
- the boot can 186 and boot 192 attachment depicted in FIG. 14 provides additional space to increase joint angle capability compared with the first embodiment since the boot head crimp is removed. Additionally, the embodiment depicted in FIGS. 13 and 14A-14C helps simplify the manufacturing process since a boot can crimping step is not required.
- a boot lower portion 195 may be directly bonded or vulcanized to the sleeve 98 along lengths L 6 and L 61 .
- a step 196 may be provided between L 6 and L 61 so that a radial height difference H results.
- the bond or vulcanization of the boot lower portion 195 to the sleeve 98 prevents the boot 192 from being lifted and/or tilted by the inside corner 148 , so that a boot clamp is not required.
- the step 196 provides increased surface area to connect the boot 192 and the sleeve 98 .
- the step 196 also provides a stop against which the boot 192 rests to prevent its movement and lock it in place.
- the boot 192 has the same profile, parts and thicknesses for the upper slope region, the concave region and the lower slope region described in FIG. 10 . This design reduces boot radial deformation, such as boot folding and self-contact, caused by high grease pressure.
- FIG. 15 depicts a sixth embodiment of a boot system 198 for the direct pinion mount joint 84 .
- the components of the joint 84 and the components of the boot system 198 are the same as those depicted in the fourth embodiment, except as follows:
- a groove 200 is located in the outer surface 156 of the sleeve 98 .
- the groove 200 extends continuously circumferentially about the outer surface 156 of the sleeve 98 at the same sleeve axial location.
- the groove 200 has a rectangular cross-section, but other shapes are permissible.
- the groove 200 is located axially adjacent L 6 .
- the groove 200 has a length L 61 , which is less than L 6 .
- the groove 200 has a depth H, which preferably is the same height H as the step in FIG. 14 .
- a boot lower portion 202 terminates in a rib 204 .
- the rib 204 preferably extends continuously circumferentially radially inward about an inside surface 206 of the boot lower portion 202 .
- the rib 204 has a complementary shape to the groove 200 and also has height H. In this embodiment, the rib 204 has a rectangular cross-section, but others are permissible.
- the groove 200 and rib 204 provide increased surface area to connect the boot 208 and the sleeve 98 .
- the groove 200 and rib 204 also function as a stop to prevent movement of the boot 208 and lock it in place.
- FIG. 16 depicts a seventh embodiment of a boot system 210 for the direct pinion mount joint 84 .
- the components of the joint 84 and the components of the boot system 210 are the same as those depicted in the fourth embodiment, except as follows.
- a groove 212 is located in the boot can angled, planar portion 116 .
- the groove 212 is located at a mid-point between the ends of the angled, planar portion 116 but it may be located at any point between the ends.
- the groove 212 creates a concave surface in an upper surface 214 of the boot can 186 and a corresponding convex surface in a lower surface 216 of the boot can 186 .
- the groove 212 preferably has the same depth as the radial height H depicted and described in FIG. 14 of the fourth embodiment.
- the inner surface 190 of the boot 192 is directly bonded or vulcanized to the boot can angled, planar portion 116 along the lower surface 216 of the boot can 110 to provide the same advantage.
- the boot lower portion 194 is similarly attached to the sleeve 54 .
- the boot 192 has the same thickness as described above for the fourth embodiment.
- the groove 212 provides increased surface area to connect the boot 192 and the boot can 186 .
- the step 196 also provides a stop against which the boot 192 rests to prevent its movement and lock it in place.
- FIGS. 17 and 17A depict a seventh embodiment of a boot system 218 utilizing the same components of the joint 84 with some of the boot system components from FIGS. 9-10 and FIG. 13 .
- the boot can 186 has the second end portion 114 with the angled, planar portion 116 .
- the boot can angled, planar portion 116 terminates in the radiused, radially outward extending end 188 , as shown in the embodiment depicted in FIG. 13 .
- the boot can angled, planar portion 116 extends for length L 7 .
- the inner surface 190 of the boot 192 is directly bonded or vulcanized to the boot can angled, planar portion 116 at least partially along L 7 .
- the boot can 186 and the above-described method of attaching the boot 192 provides additional space to increase joint angle capability compared with the first embodiment since the boot head crimp is removed. Additionally, this design helps simplify the manufacturing process since a boot can crimping step is not required.
- FIG. 17 shows a lower slope region 134 transitioning to the boot clamping portion 143 as described and depicted in FIG. 10 .
- the boot clamping portion 143 comprises three portions: L 3 , L 41 , and L 42 .
- L 3 is depicted in FIG. 17A .
- L 3 comprises the planar portion 144 on the inside surface 146 of the boot 220 .
- a press load ⁇ 1 is applied to L 3 so that L 3 is located in contact with the sleeve 98 .
- the press load ⁇ 1 also minimizes the effect, if any, of the inside corner 148 of the boot seat groove 150 that functions like a hinge.
- the first angled transition 152 separates L 3 from L 41 and L 42 .
- the first angled transition 152 has a complementary shape to the first angled transition 154 in the outer surface 156 of the sleeve 98 .
- the first angled transition 154 in the sleeve 98 leads to a sleeve groove 158 .
- a second angled transition 160 extends from the sleeve groove 158 .
- L 41 and L 42 are coplanar surfaces with one another on the inside surface 146 of the boot 220 .
- L 41 is designed to be longer than L 42 ; the two lengths being divided by line Y-Y which defines a centerline of the sleeve groove 158 . It is preferred that L 41 is longer than L 42 to help prevent region 146 from being lifted and tilted by the above-mentioned hinge.
- the thickness of the region 146 is reduced from T 35 to T 36 along L 3 . This is designed to also prevent the region 146 from being lifted and tilted by the hinge.
- a second angled transition 164 connects with the boot end portion 166 .
- L 41 and L 42 are parallel to the sleeve groove 158 . And, upon application of a clamping force, L 41 and L 42 come into contact with the sleeve groove 158 . Similarly, the first and second angled transitions 152 , 164 in the boot 220 come into contact with the first and second angled transitions 154 , 160 in the sleeve 98 upon application of the clamping force.
- FIG. 18 depicts an eighth embodiment of a boot system 222 utilizing the same components of the joint 84 with some of the boot system components from FIGS. 9-10 and FIG. 14 .
- the boot can 110 has a first end portion 112 connected to the outer race 88 and a second end portion 114 that is cantilevered over the joint 84 . More particularly, the second end portion 114 is cantilevered over a portion of the sleeve 98 .
- the second end portion 114 comprises the angled, planar portion 116 and the boot can crimp head 118 at the end of the angled, planar portion 116 .
- the boot can crimp head 118 first extends radially outward from the angled, planar portion 116 before it curves around on itself to create the semi-hemispherical hollow portion 120 .
- One end 122 of the straight portion 124 of the can 110 connects with the semi-hemispherical hollow portion 120 .
- the boot can 110 terminates at the other end of the straight portion 124 .
- the straight portion 124 is located radially inward from the angled, planar portion 116 .
- the gap 128 separates the angled planar portion 116 from the straight portion 124 .
- the boot lower portion 194 is attached to the sleeve 98 such as via a direct bond or vulcanization.
- the step 196 provides increased surface area to connect the boot 224 and the sleeve 98 and it provides a stop against which the boot 224 rests to prevent its movement and lock it in place.
- FIGS. 19 and 19A depicts a ninth embodiment of a boot system 226 utilizing the same components of the joint 84 with some of the boot system components from FIGS. 12 and 13 .
- the boot can 186 has the second end portion 114 with an angled, planar portion 116 .
- the boot can angled, planar portion 116 terminates in a radiused, radially outward extending end 188 .
- the boot can angled, planar portion 116 extends for a length L 7 .
- the inner surface 190 of the boot 228 is directly bonded or vulcanized to the boot can angled, planar portion 116 at least partially along L 7 .
- the boot 228 as depicted in FIGS. 19 and 19A has a semi-half rectangular cross section that has a thickness that gradually and smoothly decreases from the upper slope region 130 through the concave region 132 down the lower slope region 134 .
- the thickness T 31 of the upper slope region 130 is greater than the thickness T 32 of the concave region 132 , which is greater than the thickness T 33 of the lower slope region 134 .
- the boot has the straight portion L 8 between the upper slope region 130 and the lower slope region 134 .
- the straight portion L 8 is designed to maintain grease pressure in the joint 84 . Grease pressure is maintained since the boot thickness 229 along L 8 is substantially constant.
- the boot lower portion 194 may be directly bonded or vulcanized to the sleeve 98 along lengths L 6 and L 61 .
- the step 196 may be provided between L 6 and L 61 so that a radial height difference H results.
- the bond or vulcanization of the boot lower portion 194 to the sleeve 98 prevents the boot 228 from being lifted and/or tilted by the inside corner 148 , so that no boot clamp is required.
- the step 196 provides increased surface area to connect the boot 228 and the sleeve 98 .
- the step 198 also provides a stop against which the boot rests to prevent its movement and lock it in place.
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- General Engineering & Computer Science (AREA)
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- Diaphragms And Bellows (AREA)
Abstract
Description
Claims (15)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US15/404,919 US10184526B2 (en) | 2014-07-25 | 2017-01-12 | Constant velocity joint boot assembly |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
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US201462028847P | 2014-07-25 | 2014-07-25 | |
US14/703,187 US9574617B2 (en) | 2014-07-25 | 2015-05-04 | Constant velocity joint boot assembly |
US15/404,919 US10184526B2 (en) | 2014-07-25 | 2017-01-12 | Constant velocity joint boot assembly |
Related Parent Applications (1)
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US14/703,187 Continuation US9574617B2 (en) | 2014-07-25 | 2015-05-04 | Constant velocity joint boot assembly |
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US20170122379A1 US20170122379A1 (en) | 2017-05-04 |
US10184526B2 true US10184526B2 (en) | 2019-01-22 |
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US14/703,187 Active US9574617B2 (en) | 2014-07-25 | 2015-05-04 | Constant velocity joint boot assembly |
US15/404,919 Active US10184526B2 (en) | 2014-07-25 | 2017-01-12 | Constant velocity joint boot assembly |
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US14/703,187 Active US9574617B2 (en) | 2014-07-25 | 2015-05-04 | Constant velocity joint boot assembly |
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EP (1) | EP2977630B1 (en) |
JP (1) | JP5984170B2 (en) |
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TWI707002B (en) | 2016-05-25 | 2020-10-11 | 瑞士商杭斯曼高級材料公司 | Disperse azo dyes, a process for the preparation thereof and the use thereof |
CN117052806A (en) * | 2023-10-11 | 2023-11-14 | 万向钱潮股份公司 | Horn-shaped large-swing-angle dustproof part and ball cage type universal joint |
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JPH0367723U (en) | 1989-10-27 | 1991-07-02 | ||
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US5725432A (en) * | 1995-09-23 | 1998-03-10 | Gkn Automotive Ag | Constant velocity universal ball joints with window surfaces and ball surfaces having a desired roughness |
DE29823919U1 (en) | 1998-07-10 | 2000-01-20 | GKN Löbro GmbH, 63073 Offenbach | Drive arrangement with a constant velocity fixed joint and a connecting shaft |
DE19831015C1 (en) | 1998-07-10 | 2000-03-16 | Gkn Loebro Gmbh | Drive arrangement with a constant velocity fixed joint and a damping element |
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US6988949B2 (en) * | 2003-11-07 | 2006-01-24 | Gkn Driveline North America, Inc. | Constant velocity joint vent valve |
US7040992B2 (en) * | 2004-01-31 | 2006-05-09 | Gkn Driveline North America, Inc. | Boltless retention system for a constant velocity joint |
US7094155B2 (en) | 2000-12-20 | 2006-08-22 | Ntn Corporation | Constant velocity universal joint |
US7097568B2 (en) * | 2004-06-25 | 2006-08-29 | Gkn Driveline North America, Inc | Shielded sealing system for a constant velocity joint |
US7097563B2 (en) * | 2003-07-23 | 2006-08-29 | Daimlerchrysler Corporation | Constant velocity universal joint diaphragm seal |
US7229356B2 (en) | 2002-07-09 | 2007-06-12 | Showa Corporation | Boot for universal joint |
US20070173337A1 (en) * | 2006-01-26 | 2007-07-26 | Hans Wormsbaecher | Rolling boot assembly |
WO2007086172A1 (en) | 2006-01-30 | 2007-08-02 | Ntn Corporation | Constant velocity universal joint |
US7282166B2 (en) | 2004-12-22 | 2007-10-16 | Gkn Driveline North America, Inc. | Constant velocity joint plunge boot |
US7347785B2 (en) | 2005-03-24 | 2008-03-25 | American Axle & Manufacturing, Inc. | Propshaft with constant velocity joint attachment |
JP2008275133A (en) | 2007-05-07 | 2008-11-13 | Ntn Corp | Constant velocity universal joint |
JP2009115203A (en) | 2007-11-06 | 2009-05-28 | Ntn Corp | Constant velocity universal joint |
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US8012030B2 (en) * | 2008-02-14 | 2011-09-06 | Gkn Driveline Deutschland Gmbh | Connecting assembly between a shaft journal and a constant velocity universal joint |
US8070613B2 (en) * | 2008-02-14 | 2011-12-06 | Gkn Driveline Deutschland Gmbh | Connecting assembly between a shaft journal and a constant velocity joint |
US20120004044A1 (en) | 2010-06-30 | 2012-01-05 | Conger Jonathan D | Constant velocity joint with quick connector and method |
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US8342973B2 (en) * | 2009-09-30 | 2013-01-01 | Neumayer Tekfor Holding Gmbh | Sliding joint |
US20130102397A1 (en) | 2010-07-08 | 2013-04-25 | Hirokazu Ooba | Fixed-type constant velocity universal joint |
US20130252748A1 (en) * | 2012-03-22 | 2013-09-26 | Hitachi Automotive Systems Kyushu, Ltd. | Propeller Shaft and Constant Velocity Universal Joint Used Therein |
WO2014066121A1 (en) | 2012-10-26 | 2014-05-01 | Dana Automotive Systems Group, Llc | Plug-in constant velocity joint |
US8771092B2 (en) | 2009-11-25 | 2014-07-08 | Ntn Corporation | Fixed type constant velocity universal joint |
US20140213374A1 (en) * | 2011-09-23 | 2014-07-31 | Robert Leslie Cassell | High angle constant velocity joint and boot |
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JP2006090391A (en) * | 2004-09-22 | 2006-04-06 | Ntn Corp | Boot for constant velocity joint |
JP2007113613A (en) * | 2005-10-18 | 2007-05-10 | Ntn Corp | Fixed constant velocity universal joint |
DE102010001216A1 (en) * | 2009-09-16 | 2011-03-24 | Continental Teves Ag & Co. Ohg | Container, in particular for hydraulic vehicle brake systems |
US8517118B2 (en) * | 2010-06-30 | 2013-08-27 | Cnh Canada, Ltd. | Stack-fold implement having bulk fill system |
US8834279B2 (en) * | 2012-03-14 | 2014-09-16 | Dana Automotive Systems Group, Llc | Shaft assembly for a constant velocity joint |
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2015
- 2015-05-04 US US14/703,187 patent/US9574617B2/en active Active
- 2015-05-15 JP JP2015099953A patent/JP5984170B2/en not_active Expired - Fee Related
- 2015-07-23 EP EP15178150.7A patent/EP2977630B1/en active Active
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2017
- 2017-01-12 US US15/404,919 patent/US10184526B2/en active Active
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US20140213374A1 (en) * | 2011-09-23 | 2014-07-31 | Robert Leslie Cassell | High angle constant velocity joint and boot |
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Also Published As
Publication number | Publication date |
---|---|
JP5984170B2 (en) | 2016-09-06 |
EP2977630A3 (en) | 2016-07-20 |
JP2016031148A (en) | 2016-03-07 |
US9574617B2 (en) | 2017-02-21 |
US20160025151A1 (en) | 2016-01-28 |
EP2977630A2 (en) | 2016-01-27 |
US20170122379A1 (en) | 2017-05-04 |
EP2977630B1 (en) | 2019-06-05 |
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